US9523466B2 - Pressure vessel - Google Patents

Pressure vessel Download PDF

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Publication number
US9523466B2
US9523466B2 US14/414,768 US201314414768A US9523466B2 US 9523466 B2 US9523466 B2 US 9523466B2 US 201314414768 A US201314414768 A US 201314414768A US 9523466 B2 US9523466 B2 US 9523466B2
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Prior art keywords
stock
flange section
resin
pressure vessel
section
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US14/414,768
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US20150167893A1 (en
Inventor
Tadahiro Nishimoto
Yoshio Hoya
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Mitsubishi Chemical Corp
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Mitsubishi Rayon Co Ltd
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Assigned to MITSUBISHI RAYON CO., LTD. reassignment MITSUBISHI RAYON CO., LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HOYA, YOSHIO, NISHIMOTO, TADAHIRO
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Assigned to MITSUBISHI CHEMICAL CORPORATION reassignment MITSUBISHI CHEMICAL CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: MITSUBISHI RAYON CO., LTD.
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/16—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/04—Protecting sheathings
    • F17C1/06—Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/056—Small (<1 m3)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0604—Liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0612—Wall structures
    • F17C2203/0614—Single wall
    • F17C2203/0619—Single wall with two layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/066—Plastics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/0663—Synthetics in form of fibers or filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/0675—Synthetics with details of composition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0305—Bosses, e.g. boss collars
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/21—Shaping processes
    • F17C2209/2109—Moulding
    • F17C2209/2118—Moulding by injection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/21—Shaping processes
    • F17C2209/2109—Moulding
    • F17C2209/2127—Moulding by blowing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107—Single phase
    • F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/035—High pressure (>10 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/036—Very high pressure (>80 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage

Definitions

  • the present invention relates to a pressure vessel for containing gas, liquefied gas or the like, in particular, to a pressure vessel having a liner body formed by blow-molding and an FRP layer that covers an outer surface of the liner body. More particularly, the present invention relates to a pressure vessel in which a flange section of a stock overlaps an inner surface of the liner body.
  • the pressure vessel is provided with a stock that forms a gas entrance.
  • the stock is made of metal.
  • Patent Document 1 discloses a pressure vessel having a configuration in which a liner body is formed by blow-molding, and a flange section included in the stock overlaps the inner surface of the liner body.
  • FIGS. 10 and 11 are a cross-sectional view and a diagram illustrating a manufacturing process of the pressure vessel of Patent Document 1, respectively.
  • the pressure vessel 5 disclosed in Patent Document 1 has a vessel main body section constituted of a liner body 1 formed by blow-molding, an FRP layer 2 covering an outer surface of the liner body 1, and a stock 3 provided in the vessel main body section.
  • the stock 3 has a cylindrical section 3b having a gas entrance 3a and a flange section 3c that is formed to spread from a vessel inner end (a lower end in FIG. 10 ) side of the cylindrical section 3b along an inner surface of the liner body 1.
  • An adhesive resin layer 4 is interposed between the stock 3 and the liner body 1.
  • Patent Document 1 discloses that the adhesive resin layer 4 is formed of polyethylene-based thermoplastic resin to enhance the adhesive strength between the liner body 1 and the stock 3.
  • Patent Document 1 discloses the method described below, as a method of manufacturing the pressure vessel 5.
  • the stock 3 is supported by a support rod 6 and disposed between a pair of liner body molding dies 7, and a parison 9 in a cylindrical shape is suspended from the die 8 of a blow-molding machine around an outer circumferential surface of the stock 3.
  • the pair of dies 7 is clamped.
  • the parison 9 in soft state is pressed against the outer surface of the stock 3 by the die clamping.
  • the adhesive resin 4 provided on the outer surface of the stock 3 melts by heat of the parison 9, and the parison 9 and the stock 3 are bonded to each other.
  • the liner body 1 By blowing air into the parison 9 to inflate the parison 9 and press it against the inner surface of the dies 7, the liner body 1 is molded. After demolding, the outer surface of the liner body 1 is covered with fiber yarns, bundles or mats, such as carbon fiber yarns or bundles, and glass fiber yarns or bundles in which thermosetting resin such as epoxy resin and unsaturated polyester resin is impregnated, which is cured to form the FRP (CFRP, GFRP or the like) layer 2.
  • FRP CFRP, GFRP or the like
  • the pressure vessel 5 disclosed in Patent Document 1 is easily manufactured by blowing the interior of the parison 9 after disposing the stock 3 between the pair of dies 7 and clamping the dies. In this respect, it is possible to reduce the manufacturing cost, compared to the known synthetic resin pressure vessels manufactured by disposing a stock (or a cap) on the outer surface of the liner body and welding the cap on the liner body by spin-welding.
  • Patent Document 1 JP 2008-164114 A
  • the stock 3 is formed of a metal or resin.
  • the weight of the stock 3 becomes large.
  • adhesive force between the metallic stock and the resin liner body is insufficient, there is a risk of degradation of the gas sealing properties of the interface between them.
  • the rigidity of the flange section 3c is lowered.
  • the flange section 3c may bend inward to the vessel, the parison 9 may be insufficiently pressed against the flange section 3c, the adhesive strength between the liner body 1 and the stock flange section 3c may become insufficient, and the gas sealing properties of the interface between them may be lowered.
  • an object of the present invention is to provide a pressure vessel that has a blow-molded liner body and an FRP layer covering the outer surface of the liner body, in which the flange section of the stock overlaps the inner surface of the liner body, adhesive strength between the liner body and the stock flange section is high, and the gas sealing properties in the interface between them are excellent.
  • the pressure vessel includes a liner body formed by blow-molding; an FRP layer that covers an outer surface of the liner body; and a stock having a stock main body formed of metal, which has a cylindrical section that passes through the liner body and the FRP layer and an annular metal flange section that projects outward from one end of the cylindrical section in the radial direction of the cylindrical section, and a molded piece formed of a synthetic resin that covers at least an outer circumferential surface of the cylindrical section and the entire metal flange section of the stock main body, has an annular resin flange section projecting outward from the metal flange section in the radial direction, and adheres to the inner surface of the liner body, wherein the resin flange section has an upper surface, an outer circumferential end surface and a lower surface, the outer circumferential end surface is provided on an end portion of the resin flange section that faces outward in the radial direction, and the liner body continuously covers the upper surface and a part of
  • the upper surface of the resin flange section is the surface of the resin flange section that faces toward the outside of the vessel
  • the lower surface of the resin flange section is the surface of the resin flange section that faces toward the inside of the vessel.
  • the intersecting angle ⁇ between the outer circumferential end surface and the upper surface may be an acute angle.
  • the intersecting angle ⁇ may be 20° to 60°, and the height of the outer circumferential end surface may be 1 to 30 mm.
  • the molded piece may continuously cover from the lower surface of the metal flange section to the inner circumferential surface of the cylindrical section.
  • the metal flange section may be provided with a through hole through which the upper surface and the lower surface of the metal flange section communicate with each other, and the molded piece may fill the through hole.
  • the molded piece is preferably formed by injection molding.
  • the stock has a stock main body formed of metal which has a cylindrical section that passes through the liner body and the FRP layer and an annular metal flange section that projects outward from one end of the cylindrical section in the radial direction of the cylindrical section, and a molded piece made of a synthetic resin that covers at least the outer circumferential surface of the cylindrical section and the entire metal flange section of the stock main body.
  • the stock is lighter than stocks which are formed only of metal, and has strength and rigidity higher than stocks which are formed only of resin.
  • both members may firmly adhere, and it is possible to increase the gas sealing properties between the stock and the liner body (parison).
  • the surface adhering to the inner surface of the liner body is formed of the molded piece, adhesive strength between the resin liner body and the molded piece is high.
  • the gas sealing properties between the stock and the liner body increase.
  • the intersecting angle ⁇ between the outer circumferential end surface of the resin flange and the upper surface is an acute angle. For that reason, when pressing the stock against the parison, the parison bulges at the peripheral edge portion of the stock, and the bulged portion covers a part of the outer circumferential end surface. Thus, the gas sealing properties between the stock and the liner body (parison) increase.
  • the outer circumferential portion of the flange section (resin flange section) of the stock has an outer circumferential end surface, strength and rigidity of the outer circumferential end portion of the stock are high.
  • the outer circumferential end portion of the stock is prevented from bending in a direction inward of the vessel. Therefore, the adhesive strength between the parison and the stock increases, and the gas sealing properties between the stock and the liner body (parison) increase.
  • the molded piece covers at least the outer circumferential surface of the cylindrical section and the overall metal flange section of the stock main body.
  • the metal flange section is present in the flange section of the stock, the strength and rigidity of the flange section of the stock increase.
  • the molded piece further continuously covers from the lower surface of the metal flange section to the inner circumferential surface of the cylindrical section. This makes it possible to improve the integrity between the molded piece and the metal stock main body.
  • the lower surface of the metal flange section is the surface of the metal flange section that faces toward the inside of the vessel.
  • the stock main body has a cylindrical section which passes through the liner body and the FRP layer, and an annular metal flange section that protrudes outward from one end of the cylindrical section in the radial direction of the cylindrical section. Furthermore, the metal flange section is provided with a through hole through which the outer surface and the inner surface of the metal flange section communicate with each other, and the molded piece fills the through hole. Thus, the molded piece on the outer surface and the molded piece on the inner surface of the metal flange section are connected to each other, which makes it possible to improve the integrity between the metal stock main body and the molded piece.
  • FIG. 1 is a cross-sectional view illustrating a structure of a stock used in a pressure vessel according to a first embodiment of the present invention
  • FIG. 2 is a cross-sectional view illustrating a structure near the stock of the pressure vessel according to the first embodiment of the present invention
  • FIG. 3 is an enlarged view near a leading end of a stock flange section illustrated in FIG. 2 ;
  • FIG. 4 is a cross-sectional view illustrating a method of manufacturing the pressure vessel according to the first embodiment of the present invention
  • FIG. 5 is a cross-sectional view illustrating a structure of a stock used for a pressure vessel according to a second embodiment of the present invention
  • FIG. 6 is a cross-sectional view illustrating a structure of a stock used for a pressure vessel according to a third embodiment of the present invention.
  • FIG. 7 is a cross-sectional view illustrating a structure of a stock used for a pressure vessel according to a fourth embodiment of the present invention.
  • FIG. 8 is a cross-sectional view illustrating a structure of a stock used for a pressure vessel according to a fifth embodiment of the present invention.
  • FIG. 9 is a cross-sectional view illustrating a structure of a stock used for a pressure vessel according to a sixth embodiment of the present invention.
  • FIG. 10 is a cross-sectional view illustrating a structure near a stock of a conventional pressure vessel.
  • FIG. 11 is a cross-sectional view illustrating a method of manufacturing the conventional pressure vessel illustrated in FIG. 10 .
  • FIGS. 1 to 4 illustrate a pressure vessel according to first to fourth embodiments of the present invention and a manufacturing method thereof.
  • a pressure vessel 10 illustrated in FIG. 2 has a blow-molded liner body 11 , an FRP layer 12 that covers the outer surface of the liner body 11 , and a stock 20 having a flange section 21 that adheres to the inner surface of the liner body 11 .
  • the stock 20 penetrates the liner body 11 and the FRP layer 12 , has a stock main body 30 made of metal having a gas entrance 31 , and has a molded piece 40 made of synthetic resin that covers an outer circumference of the stock main body 30 .
  • an external shape of a top end portion (outer end portion of the vessel) 23 of the stock 20 is a hexagonal shape to be able to be hooked with a tool such as a wrench or the like.
  • the stock main body 30 has a cylindrical section 32 that forms the gas entrance 31 and passes through the interior and exterior of the pressure vessel 10 in a cylindrical axial direction, and an annular metal flange section 33 that protrudes outward in radial directions of the cylindrical section 32 from the end (lower end) of the cylindrical section 32 in the vessel.
  • the molded piece 40 continuously covers the outer circumferential surface of the cylindrical section 32 , the upper surface (the surface facing the liner body) of the metal flange section 33 , the leading end of the metal flange section 33 , and the lower surface (the surface of the opposite side of the upper surface) of the metal flange section 33 .
  • the molded piece 40 covers the upper end surface (the end surface of the vessel outside) of the cylindrical section 32 of the stock main body 30 , and has an inner circumferential surface section 47 that continuously covers from the lower surface of the metal flange section 33 to the inner circumferential surface of the gas entrance 31 via the edge portion of the gas entrance 31 .
  • an elongated convexity 35 inward in the radial direction of the stock main body 30 is annularly disposed at an intermediate portion in the cylinder axial direction.
  • the inner circumferential surface section 47 of the molded piece 40 covers the inner circumferential surface of the gas entrance 31 from the elongated convexity 35 toward the vessel inside (the lower end of the cylindrical section 32 ).
  • a female screw 36 is formed on the inner circumferential surface of the gas entrance 31 from the elongated convexity 35 toward the vessel outside, and a gas supplying and extracting valve or the like can be attached thereto by screwing.
  • the molded piece 40 is equipped with an annular resin flange section 42 that projects outward from the metal flange section 33 in the radial direction of the metal flange section 33 .
  • the resin flange section 42 is formed of the upper surface, the outer circumferential end surface 43 and the lower surface, and has a predetermined thickness.
  • the upper surface of the resin flange section 42 is formed to be the same surface as the upper surface of the top surface section 41 that covers the upper surface of the metal flange section 33 .
  • the outer circumferential end surface 43 is provided at the end portion of the resin flange section 42 that faces outward in the radial direction. It is preferable that the height H of the outer circumferential end surface 43 be 1 to 30 mm, and particularly 3 to 20 mm.
  • the height H of the outer circumferential end surface 43 refers to a distance between the upper surface of the resin flange section 42 (the top surface of the top surface section 41 ) and the lower end of the outer circumferential end surface 43 (the tangent of the end portions of the outer circumferential end surface 43 and the lower surface of the resin flange section 42 ).
  • An intersecting angle ⁇ between the outer circumferential end surface 43 and the upper surface of the resin flange section 42 (the top surface of the top surface section 41 ) is preferably 10° to 85°, more preferably 20 to 60°, and particularly preferably 20° to 45°.
  • a groove 44 is annularly provided on the lower surface of the resin flange section 42 .
  • the pressure vessel of the present invention is not limited to a configuration in which the groove is provided on the lower surface of the resin flange as in this embodiment, and the groove need not be provided on the lower surface of the resin flange.
  • the molded piece 40 is continuously formed from the lower end surface of the stock main body 30 to the molded piece inner circumferential surface section 47 via the corner edge of the gas entrance 31 .
  • the molded piece 40 covers from the outer circumferential surface to the upper end surface of the cylindrical section 32 of the stock main body 30 .
  • a step section 46 for mounting a seal ring such as an O-ring is provided on the inner circumferential corner edge of the top section 49 forming the upper end surface portion of the molded piece.
  • the molded piece 40 is preferably formed by injection-molding.
  • the stock 20 is manufactured by molding the molded piece 40 by insert-molding following disposing the stock main body 30 within the injection-molding dies.
  • a pressure vessel 10 using a stock 20 is manufactured as follows. As illustrated in FIG. 4 , the stock 20 is disposed between a pair of blow-molding dies 51 so as to be supported by a support rod 52 , a cylindrical parison 55 is extruded from a circular die 54 , and the stock 20 is surrounded by the parison 55 .
  • the dies 51 and 51 are clamped to press the parison 55 against the outer surface of the stock 20 .
  • the liner body 11 is blow-molded by blowing gas such as air into the parison 55 to inflate the parison 55 and to press the parison 55 against the inner surface of the dies 51 and 51 .
  • the liner body 11 with the stock 20 is demolded, and thereafter, the FRP layer is formed on the outer circumferential surface of the liner body 11 by a filament winding method, a tape winding method, or the like.
  • the strength and rigidity of the pressure vessel 10 increase. Since the resin flange section 42 protruding outward from the metal flange section 33 has a large thickness H, the strength and rigidity are high.
  • the flange section 21 bites into the parison 55 , a part of the liner body 11 formed from the parison 55 bulges along the outer circumferential end surface 43 of the resin flange section 42 as illustrated in FIG. 3 , and the bulged portion 11 t covers a part of the outer circumferential end surface 43 .
  • the penetration of gas from the pressure vessel 10 to the interface between the resin flange section 42 of the molded piece 40 and the liner body 11 is prevented, and thus, the gas sealing properties of the interface are improved.
  • the intersecting angle ⁇ between the upper surface of the resin flange section 42 and the outer circumferential end surface 43 thereof is an acute angle
  • a structure is achieved in which the acute angle section of the leading edge of the flange section 42 is interposed between the solidified bulged portion 11 t and the liner body 11 formed on the upper side of the resin flange section 42 .
  • the strength of the joint between the resin flange section 42 and the liner body 11 is enhanced.
  • the stock 20 is lighter than a cap formed of only metal, the strength and rigidity thereof including the resin flange section 42 are high as described above, and the liner body 11 and the molded piece 40 firmly coheres with each other. Therefore, the strength of the joint between the liner body 11 and the molded piece 40 is high, and the gas sealing properties of the interface between the liner body 11 and the molded piece 40 are very good. Furthermore, since the liner body 11 has the bulged portion 11 t that covers a part of the outer circumferential end surface 43 , the interface between the liner body 11 and the resin flange section 42 is covered by the bulged portion 11 t . Therefore, the pressure vessel 10 has excellent gas sealing properties at the interface.
  • the molded piece 40 has an inner circumferential surface section 47 that continuously covers from the lower surface of the stock main body 30 (metal flange section 33 ) to the inner circumferential surface of the gas entrance 31 (cylindrical section 32 ). In this case, integrity between the molded piece 40 and the stock main body 30 is high, and the gas sealing properties of the interface between the molded piece 40 and the stock main body 30 are excellent.
  • FIGS. 5 to 9 Stocks used for pressure vessels according to other embodiments of the present invention are illustrated in FIGS. 5 to 9 .
  • FIG. 5 illustrates a stock 20 A used in a pressure vessel according to the second embodiment of the present invention.
  • the stock 20 A illustrated in FIG. 5 is equipped with a metal ring 60 that is formed of a brass or the like and provided on the upper side of the molded piece top section 49 that covers the upper end surface of the stock main body 30 .
  • the top surface of the molded piece top section 49 is a plane, and a seal ring installation section 61 for an O-ring or the like is formed on the inner side of the inner circumferential surface of the metal ring 60 and on the top surface of the molded piece top section 49 .
  • the elongated convexity 35 of the inner circumferential surface of the gas entrance 31 illustrated in the above-described first embodiment is not provided.
  • the molded piece 40 is not provided with the inner circumferential surface section 47 that covers the inner circumferential surface of the gas entrance 31 .
  • Other configurations are the same as those of the stock 20 , and the same reference numerals designate the same parts.
  • the metal ring 60 may be integrated with the molded piece 40 by insert-molding and may be bonded to the molded piece top section 49 with an adhesive.
  • FIG. 6 illustrates a stock 20 B used in a pressure vessel according to the third embodiment of the present invention.
  • the stock 20 B illustrated in FIG. 6 has an elongated convexity 48 that is annularly provided on the top surface of the molded piece top section 49 configured to cover the upper end surface of the stock main body 30 , and a metal ring 60 that is provided on the outer circumferential side of the elongated convexity 48 . Furthermore, a seal ring installation section 61 is provided on the inner circumferential side of the elongated convexity 48 .
  • Other configurations are the same as those of the second embodiment, and the same reference numerals designate the same parts.
  • FIG. 7 illustrates a stock 20 C used in a pressure vessel according to the fourth embodiment of present the invention.
  • the stock 20 C illustrated in FIG. 7 is not provided with the molded piece top section 49 illustrated in the above-described first to third embodiments.
  • an O-ring is mounted to an outer circumferential surface of a leading end portion of a valve to be inserted into the gas entrance 31 , and is made come into contact with the inner circumferential surface section 47 of the mold piece in a freely slidable manner.
  • Other configurations are the same as those of the stock 20 , and the same reference numerals designate the same parts.
  • FIG. 8 illustrates a stock 20 D used in a pressure vessel according to the fifth embodiment of the present invention.
  • the stock 20 D illustrated in FIG. 8 has unevenness 41 a formed on the top surface section 41 of the molded piece 40 . This makes it possible to further enhance the adhesive strength between the molded piece 40 and the liner body 11 .
  • Other configurations are the same as those of the stock 20 , and the same reference numerals designate the same parts.
  • FIG. 9 illustrates a stock 20 E used in a pressure vessel according to the sixth embodiment of the invention.
  • the stock 20 E illustrated in FIG. 9 has an outermost circumferential section (resin flange section 42 ) of the molded piece 40 having a triangular cross-sectional shape. That is, in each of the above-described caps 20 and 20 A to 20 D, the lower end of the outer circumferential end surface 43 and the groove 44 are slightly spaced from each other, but in the stock 20 E of FIG. 9 , the lower end of the outer circumferential end surface 43 reaches the beginning corner edge of the groove 44 .
  • Other configurations are the same as those of the stock 20 , and the same reference numerals designate the same parts.
  • the metal flange section 33 may be provided with a through hole 65 (indicated with broken lines in FIG. 9 ) through which the upper surface and the lower surface of the metal flange section communicate with each other. Furthermore, by filling the through hole 65 with the mold piece 40 , the top surface section 41 and the molded piece on the lower surface side of the metal flange section 33 may be connected to each other with the molded piece 40 filling the through hole 65 .
  • the outer circumferential surface of the cylindrical section 32 of the stock main body 30 need not be covered by the molded piece 40 .
  • the surface of the stock main body 30 may be roughened by sand-blasting, shot-blasting, cutting process or the like, and may be subjected to various surface treatments.
  • polyolefin resins such as high-density polyethylene-based resin, cross-linked polyethylene, polypropylene resin, and cyclic olefin-based resin
  • polyamide-based resins such as nylon 6, nylon 6, 6, nylon 11 and nylon 12
  • polyester-based resins such as poly(ethylene terephthalate) and poly(butylene terephthalate)
  • engineering plastics such as acrylonitrile-butadiene-styrene copolymer (ABS) resin
  • ABS acrylonitrile-butadiene-styrene copolymer
  • the material of the liner body 11 is not limited to the materials described above.
  • the liner body 11 may be constituted by a single layer body, a multi-layer body, or a composite material of the above-described thermoplastic resin.
  • the liner body may be formed of a composite material in which gas barrier resin such as a engineering plastic, ethylene-(vinyl alcohol) copolymer (EVOH) or poly(vinyl alcohol) (PVA) resin, elastomer, a metal member or an inorganic filler is dispersed in the high-density polyethylene-based resin layer, and as a structure of the liner body 11 , a laminate having a multi-layer structure containing at least a thermoplastic resin layer/an adhesive layer/a barrier layer may be used.
  • gas barrier resin such as a engineering plastic, ethylene-(vinyl alcohol) copolymer (EVOH) or poly(vinyl alcohol) (PVA) resin, elastomer, a metal member or an inorganic filler is dispersed in the high-density polyethylene-based resin layer, and
  • PA polyamide
  • PET poly(ethylene terephthalate)
  • PBT poly(butylene terephthalate)
  • AS acrylonitrile-butadiene-styrene copolymer
  • PC polycarbonate
  • POM polyacetal
  • PPE poly(phenylene ether)
  • PPS poly(phenylene sulfide)
  • aromatic polyester resin liquid crystal resin
  • talc silica, calcium carbonate, mica or the like
  • fine powder talc or fine powder mica having a plate-like crystal structure having an average particle size of 0.5 to 10 ⁇ m is preferred to others.
  • thermoplastic resin layer such as the above-described high-density polyethylene/an adhesive layer/a barrier layer, a three-kind five-layer structure of a thermoplastic resin layer/an adhesive layer/a barrier layer/an adhesive layer/a thermoplastic resin layer, a laminate having three or more layers, such as a four-kind six-layer structure of a thermoplastic resin layer/a recycled resin layer/an adhesive layer/a barrier layer/an adhesive layer/a thermoplastic resin layer and a two-kind two-layer of a thermoplastic resin layer/an adhesive layer or the like can be exemplified.
  • polyamide resin polyamide resin
  • polyester resin ethylene-(vinyl alcohol) copolymer
  • poly(vinyl alcohol) resin polyacrylonitrile resin or the like
  • polyamide resin polyamide resin
  • polyester resin ethylene-(vinyl alcohol) copolymer
  • poly(vinyl alcohol) resin polyacrylonitrile resin or the like
  • any one of helical winding, hoop winding, label winding may be adopted, and a combination thereof may be used.
  • the winding method specifically, for example, there is a method for winding while loading the resin to the reinforcing fiber (bundle) during the winding process or a method for winding the reinforcing fiber (bundle) impregnated with resin in advance (prepreg).
  • the FRP layer may be formed by other methods, such as a prepreg method in which a continuous reinforcing material such as fabrics is formed after being impregnated with thermosetting resin.
  • the reinforcing fiber for forming the FRP layer carbon fiber, glass fiber, organic high-modulus fiber (for example, aramid fiber, ultra-high-strength polyester fiber), metal fiber, ceramic fiber or the like can be exemplified, and it is also possible to use one kind thereof or two or more kinds thereof in combination.
  • thermosetting or photo-curable resins such as epoxy resin, unsaturated polyester resin, urea resin, phenolic resin, melamine resin, polyurethane resin, polyimide resin and vinyl ester resin, polyamide resin, polyester resins such as poly(ethylene terephthalate) and poly(butylene terephthalate), engineering plastic such as ABS resin, poly(ether ketone), and poly(phenylene sulfide) and thermoplastic resins such as polypropylene and poly-4-methyl-1-pentene resin can be exemplified.
  • metal constituting the stock main body 30 iron, aluminum, copper, nickel, titanium or alloys thereof (for example, brass) can be exemplified, but the metal is not limited thereto.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Laminated Bodies (AREA)
US14/414,768 2012-07-18 2013-07-18 Pressure vessel Active US9523466B2 (en)

Applications Claiming Priority (3)

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JP2012159638 2012-07-18
JP2012-159638 2012-07-18
PCT/JP2013/069495 WO2014014049A1 (fr) 2012-07-18 2013-07-18 Cuve sous pression

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US20150167893A1 US20150167893A1 (en) 2015-06-18
US9523466B2 true US9523466B2 (en) 2016-12-20

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US (1) US9523466B2 (fr)
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JP (3) JP5928473B2 (fr)
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US10816138B2 (en) 2017-09-15 2020-10-27 Goodrich Corporation Manufacture of a conformable pressure vessel
US11091266B2 (en) 2017-08-29 2021-08-17 Goodrich Corporation Conformable tank fabricated using additive manufacturing
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JP2016017545A (ja) * 2014-07-07 2016-02-01 株式会社Fts 圧力容器
WO2016009288A1 (fr) * 2014-07-17 2016-01-21 Faber Industrie S.P.A. Récipient sous pression
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KR102201792B1 (ko) * 2018-11-30 2021-01-12 롯데케미칼 주식회사 압력용기용 보스 및 이를 구비한 압력용기
JP7338575B2 (ja) * 2020-07-08 2023-09-05 トヨタ自動車株式会社 高圧タンク
CN111963890B (zh) * 2020-08-28 2022-07-15 亚普汽车部件股份有限公司 一种高压复合容器
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Publication number Priority date Publication date Assignee Title
US10703481B2 (en) 2017-08-29 2020-07-07 Goodrich Corporation Conformable tank with sandwich structure walls
US11091266B2 (en) 2017-08-29 2021-08-17 Goodrich Corporation Conformable tank fabricated using additive manufacturing
US11939105B2 (en) 2017-08-29 2024-03-26 Goodrich Corporation 3D woven conformable tank
US10816138B2 (en) 2017-09-15 2020-10-27 Goodrich Corporation Manufacture of a conformable pressure vessel
US11725779B2 (en) 2017-09-15 2023-08-15 Goodrich Corporation Manufacture of a conformable pressure vessel

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WO2014014049A1 (fr) 2014-01-23
JPWO2014014049A1 (ja) 2016-07-07
JP2015017709A (ja) 2015-01-29
EP2876351A4 (fr) 2015-10-28
JP5928473B2 (ja) 2016-06-01
JP2017072264A (ja) 2017-04-13
JP6409887B2 (ja) 2018-10-24
US20150167893A1 (en) 2015-06-18
EP2876351A1 (fr) 2015-05-27

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